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1. 发明申请

US20180257756A1 VIRTUAL AERODYNAMIC SURFACE SYSTEMS 审中-公开
公开(公告)号：US20180257756A1
公开(公告)日：2018-09-13
申请号：US15977174
申请日：2018-05-11
申请人： ROHR, INC.
发明人： Teresa M. Kruckenberg , Vijay V. Pujar , Robert L. Braden
IPC分类号： B64C1/38 , B64C21/00 , B64C23/00
CPC分类号： B64C1/38 , B64C21/00 , B64C23/005 , B64C2220/00 , B64C2230/02 , Y02T50/166
摘要： A method of generating a pressure wave proximate an airflow surface and altering airflow to promote a localized lowering of skin friction over the airflow surface is described herein. A series of pressure waves may be configured to create a virtual riblet to control turbulent vortices in a boundary layer adjacent to the airflow surface creating a virtual riblet. The pressure waves may be configured to prevent disruption of the flow of air relative to at least one of a step or a gap associated with the airflow surface. The pressure wave generating system may be comprised of at least one of a thermoacoustic material, a piezoelectric material and a semiconductor material, and a microelectric circuit.

2. 发明申请

US20180186478A1 INTEGRATED ABLATIVE HEAT SHIELD 审中-公开
公开(公告)号：US20180186478A1
公开(公告)日：2018-07-05
申请号：US15813343
申请日：2017-11-15
申请人： NATIONAL CHUNG SHAN INSTITUTE OF SCIENCE AND TECHNOLOGY
发明人： MAU-YI HUANG , REN-SO DENG , GENG-WEN CHANG , DAR-PING JUANG , CHENG-HUAN WANG
IPC分类号： B64G1/58 , B64C1/38 , B29C70/08
CPC分类号： B64G1/58 , B29C65/02 , B29C66/1282 , B29C66/1284 , B29C66/1286 , B29C66/543 , B29C66/7212 , B29C66/73754 , B29C70/081 , B32B2307/304 , B32B2307/3065 , B32B2605/18 , B64C1/38 , B64C30/00
摘要： An integrated heat shield which encloses a frame structure comprises a leading edge component, a left side component, a right side component, an optionally top component, an optional bottom component and an optional trailing edge subassembly, wherein the leading edge component and the left and right side components are directly, integrally co-cured on the frame structure while in a B-stage. The leading edge component and the left and right side components are shingle laminated to form ply angles to air flow. The leading edge component and the side components are scarf-jointed or step-jointed. The side components and trailing edge subassembly are also scarf jointed or step-jointed. The co-curing as well as the scarf or step joints makes the heat shield an integrated assembly. A method of manufacturing the integrated heat shield is further introduced.

3. 发明申请

US20170113245A1 METHODS AND SYSTEMS FOR APPLYING AERODYNAMICALLY FUNCTIONAL COATINGS TO A SURFACE 审中-公开
公开(公告)号：US20170113245A1
公开(公告)日：2017-04-27
申请号：US15206322
申请日：2016-07-11
申请人： The Boeing Company
发明人： Douglas H. Berry , Scott A. Davis
IPC分类号： B05D1/32 , B64C1/38 , B05D5/00 , B05D7/00 , B05D3/10
CPC分类号： B05D1/32 , B05D3/108 , B05D3/12 , B05D5/00 , B05D5/065 , B05D7/57 , B05D2202/00 , B64C1/38 , B64C3/36 , B64C5/02 , B64C7/02 , B64C23/065 , Y10T428/24628
摘要： An aero-contoured coating system is provided. The system has an aerodynamically functional coating having at least one or more color layers, one or more first clearcoat layers over the color layer(s) to obtain a pre-aero-contoured coating, the one or more first clearcoat layers configured for abrasion and aero-contouring to obtain an aero-contoured surface, and one or more additional clearcoat layers over the aero-contoured surface. The system further has a structure having a prepared and primed substrate surface with a primer layer. The system further has an aero-contouring device to abrade a plurality of flow surfaces on a pre-aero-contoured coated surface and to mechanically aero-contour a plurality of coating edges to reduce one or more coating edge peaks and coating edge angles of abutting coating edges between the one or more color layers. The system further has one or more masking elements for masking the one or more color layers.

4. 发明申请

US20160265133A1 METHOD FOR MANUFACTURING AN AIRCRAFT COMPONENT EQUIPPED WITH A PROTECTION AGAINST ABRASION AND HEAT, AND AIRCRAFT COMPONENT MANUFACTURED THROUGH SAID METHOD 审中-公开
标题翻译：装备有防磨损保护装置的飞机部件的制造方法以及通过上述方法制造的飞机部件
公开(公告)号：US20160265133A1
公开(公告)日：2016-09-15
申请号：US15036010
申请日：2014-11-10
申请人： ALENIA AERMACCHI S.P.A.
发明人： Luca BOTTERO , Massimo GREGORI
IPC分类号： C25D5/54 , B64C1/38 , C25D3/12 , C25D3/56 , C25D7/00 , C25D21/12
CPC分类号： C25D5/54 , B64C1/38 , B64C3/36 , B64C2001/0072 , B64C2001/0081 , C25D3/12 , C25D3/562 , C25D7/00 , C25D21/12
摘要： A method includes providing an aircraft component including a substrate made of composite material and a polymeric matrix; and applying a protective coating made of metallic material to the substrate. The protective coating is applied to the polymeric matrix by an electrolytic deposition process.
摘要翻译：一种方法包括提供包括由复合材料制成的基底和聚合物基体的飞行器部件; 并将由金属材料制成的保护涂层施加到基底上。通过电解沉积工艺将保护涂层施加到聚合物基质上。

5. 发明申请

US20160194069A1 THERMALLY CONDUCTIVE UNMANNED AERIAL VEHICLE AND METHOD OF MAKING SAME 审中-公开
标题翻译：导热式无人驾驶航空器及其制造方法
公开(公告)号：US20160194069A1
公开(公告)日：2016-07-07
申请号：US14881117
申请日：2015-10-12
申请人： Rapid Unmanned Aerial Systems, LLC
发明人： Alan TAYLOR
IPC分类号： B64C1/38 , B64C27/08 , B64F5/00 , B64C39/02
CPC分类号： B64C1/38 , B64C27/08 , B64C39/024 , B64C2001/0054 , B64C2001/0072 , B64C2201/027 , B64C2201/042 , B64F5/10 , Y02T50/43
摘要： An unmanned aerial vehicle includes a body and a heat source disposed in the body. The heat source includes at least one of an electronic controller system and a motor. The unmanned aerial vehicle further includes a plurality of rotor blades. At least a portion of the body is constructed of crystalline carbon fibers.
摘要翻译：无人驾驶飞行器包括设置在车体中的主体和热源。热源包括电子控制器系统和电动机中的至少一个。无人飞行器还包括多个转子叶片。身体的至少一部分由结晶碳纤维构成。

6. 发明授权

US09290261B2 Method and assembly for attaching components 有权
标题翻译：用于连接组件的方法和装配
公开(公告)号：US09290261B2
公开(公告)日：2016-03-22
申请号：US13157284
申请日：2011-06-09
申请人： Wendell V. Twelves , Kathleen E. Sinnamon
发明人： Wendell V. Twelves , Kathleen E. Sinnamon
IPC分类号： F16B1/00 , B64C9/02 , F16B5/02
CPC分类号： F16B5/0241 , B64C1/06 , B64C1/38 , B64C9/02 , B64F5/00 , Y10T29/49826 , Y10T403/21 , Y10T403/217
摘要： An example adjustable linking member of a mounting assembly includes a first attachment portion and a second attachment portion. The first attachment portion connects a linking member to a first component. The second attachment portion connects the linking member to a second component. A variable portion of the adjustable linking member varies a distance between the first attachment portion and the second attachment portion in a first direction when heated. The variable portion varies the distance between the first attachment portion and the second attachment portion in a second direction when cooled. The first direction is opposite the second direction.
摘要翻译：安装组件的示例性可调连接构件包括第一附接部分和第二附接部分。第一附接部分将连接部件连接到第一部件。第二附接部分将连接部件连接到第二部件。可调连接构件的可变部分在加热时在第一方向上改变第一附接部分和第二附接部分之间的距离。当冷却时，可变部分在第二方向上改变第一附接部分和第二附接部分之间的距离。第一个方向与第二个方向相反。

7. 发明授权

US09193457B2 Superconductive hypersonic liquefaction nosecone 有权
标题翻译：超导超声液化诺西酮
公开(公告)号：US09193457B2
公开(公告)日：2015-11-24
申请号：US13969467
申请日：2013-08-16
申请人： Charl Emelio Janeke
发明人： Charl Emelio Janeke
IPC分类号： B64C30/00 , B64C1/00 , B64C1/38
CPC分类号： B64C1/38 , B64C1/0009 , B64C23/04 , B64C30/00 , B64C2001/0045 , B64D27/023
摘要： An apparatus and method for mitigating the shock front of an aerospace plane flying at hypersonic speeds. The invention employs supercooling driven by the cryogenic power of liquid hydrogen, regenerative evaporation of liquid hydrogen or liquid nitrogen and consequential isothermal compression, to usurp the shock front in totality at Mach 1.
摘要翻译：一种减轻超音速飞行的航空航天飞机的冲击前沿的装置和方法。本发明采用由液氢的低温动力驱动的过冷，液态氢或液氮的再生蒸发和随后的等温压缩，以Mach 1全面篡夺冲击前沿。

8. 发明申请

US20140329055A1 METHODS AND SYSTEMS FOR APPLYING AERODYNAMICALLY FUNCTIONAL COATINGS TO A SURFACE 有权
标题翻译：将空气动力学功能涂层应用于表面的方法和系统
公开(公告)号：US20140329055A1
公开(公告)日：2014-11-06
申请号：US13875774
申请日：2013-05-02
申请人： The Boeing Company
发明人： Douglas H. Berry , Scott A. Davis
IPC分类号： B05D1/32
CPC分类号： B05D1/32 , B05D3/108 , B05D3/12 , B05D5/00 , B05D5/065 , B05D7/57 , B05D2202/00 , B64C1/38 , B64C3/36 , B64C5/02 , B64C7/02 , B64C23/065 , Y10T428/24628
摘要： A method for applying an aerodynamically functional coating to an exterior surface is provided. The method includes preparing an uncoated substrate surface to obtain a prepared substrate surface; applying a primer on the prepared substrate surface to obtain a primed substrate surface with a primer layer; applying and curing a basecoat field color to obtain a basecoat field color layer; masking for a basecoat design color on the basecoat field color layer; applying and curing the basecoat design color to obtain a first basecoat design color layer; masking for, applying, and curing any subsequent basecoat design color layers on the basecoat field color layer; applying and curing a clearcoat to obtain a first clearcoat layer; mechanically aero-contouring a plurality of coating edges to obtain an aero-contoured surface; and, applying additional clearcoat to obtain one or more additional clearcoat layers.
摘要翻译：提供了一种将空气动力学功能涂层施加到外表面的方法。该方法包括制备未涂覆的基底表面以获得制备的基底表面; 在制备的基材表面上施加底漆以获得具有底漆层的底漆底漆表面; 施加和固化底漆场颜色以获得底漆场色层; 在底漆场彩色层上掩饰底漆设计颜色; 应用和固化底漆设计颜色，以获得第一个底漆设计色层; 掩蔽，涂抹和固化底漆色彩层上任何后续的底漆设计色层; 施加和固化透明涂层以获得第一透明涂层; 机械空气轮廓化多个涂层边缘以获得航空轮廓表面; 并施加额外的透明涂层以获得一个或多个另外的清漆层。

9. 发明授权

US08678316B2 Amorphous metal riblets 有权
标题翻译：无定形金属肋
公开(公告)号：US08678316B2
公开(公告)日：2014-03-25
申请号：US12361918
申请日：2009-01-29
申请人： Diane C. Rawlings , Stephen Christensen
发明人： Diane C. Rawlings , Stephen Christensen
IPC分类号： B64C1/38 , B64C21/10
CPC分类号： B64C21/10 , B32B3/08 , B32B3/30 , B32B7/12 , B32B15/08 , B32B15/20 , B32B25/08 , B32B27/283 , B32B27/288 , B32B27/34 , B32B27/38 , B32B27/40 , B32B2250/02 , B32B2307/416 , B32B2307/50 , B32B2307/702 , B32B2605/18 , B64C1/38 , B64C2230/26 , F15D1/0035 , F15D1/004 , Y02T50/166 , Y10T428/24355 , Y10T428/24612
摘要： An array of aerodynamic riblets is created by a plurality of high stiffness tips with a layer supporting the tips in predetermined spaced relation and adhering the tips to a vehicle surface.
摘要翻译：空气动力肋的阵列由多个高刚度尖端产生，其具有以预定的间隔关系支撑尖端的层并且将尖端附接到车辆表面。

10. 发明申请

US20110253344A1 Protective structure 审中-公开
标题翻译：防护结构
公开(公告)号：US20110253344A1
公开(公告)日：2011-10-20
申请号：US13068299
申请日：2011-05-05
申请人： Markus Kuhn , Hermann Hald , Waldemar Rotaermel
发明人： Markus Kuhn , Hermann Hald , Waldemar Rotaermel
IPC分类号： F28D15/04 , F28D15/00
CPC分类号： B64C1/38 , B64C3/36 , B64G1/58
摘要： A protective structure, comprising a first material region having a surface facing the exterior and an inner boundary surface, wherein channels for conducting fluid are disposed between the outer surface and the inner boundary surface, and a second material region, which is thermally connected at least in sub-regions to the inner boundary surface of the first material region and which is porous, wherein in pores a reaction medium and/or cooling medium is stored and channels for conducting fluid extend as far as the inner boundary surface of the first material region.
摘要翻译：一种保护结构，包括具有面向外部的表面的第一材料区域和内部边界表面，其中用于传导流体的通道设置在外表面和内边界表面之间，第二材料区域至少热连接在所述第一材料区域的内边界的子区域中，并且是多孔的，其中在孔中存储有反应介质和/或冷却介质，并且用于导电流体的通道延伸到所述第一材料区域的内边界表面。

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